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Rev. 11/15/02 #41 Continental Flight Manual
Wing Anti-Ice Panel
< Wing Anti-Ice VALVE OPEN Lights
Illuminated (blue) –
· Bright – Related wing anti-ice control valve is in transit, or, related
wing anti-ice control valve position disagrees with WING ANTI–ICE
switch position.
· Dim – Related wing anti-ice control valve is open (switch ON).
· Extinguished – Related wing anti-ice control valve is closed (switch
OFF).
= WING ANTI–ICE Switch
OFF – Wing anti-ice control valves are closed.
ON (in the air) –
· Wing anti-ice control valves are open
BCD
· Stick shaker logic is set for icing conditions.
· Stick shaker logic remains set for icing conditions for the remainder of
the flight, regardless of subsequent WING ANTI-ICE switch position.
ANTI-ICE & RAIN
737 Sec. 6.3 Page 17
Flight Manual Continental Rev. 11/15/02 #41
ON (on the ground) –
· Wing anti-ice control valves open if thrust on both engines is below
takeoff warning setting and temperature inside both distribution ducts
is below thermal switch activation temperature.
· Control valves close if either engine thrust is above takeoff warning
setting or thermal switch is activated in either distribution duct.
Switch remains ON.
· Switch trips OFF at lift-off.
ANTI-ICE & RAIN
Sec. 6.3 Page 18 737
Rev. 11/15/02 #41 Continental Flight Manual
PROBE AND SENSOR HEAT
Pitot probes, the total air temperature probe and the alpha vanes are electrically
heated. Static ports are not heated.
>>@ Probe, Alpha Vane And Static Port Locations
ANTI-ICE & RAIN
737 Sec. 6.3 Page 19
Flight Manual Continental Rev. 11/15/02 #41
BCD Probe And Sensor Locations
Note: Static ports (4), located on the fuselage, are not heated.
ANTI-ICE & RAIN
Sec. 6.3 Page 20 737
Rev. 11/15/02 #41 Continental Flight Manual
>>@ Probe Heat Panel
< Probe Heat Lights
Illuminated (amber) – related probe not heated.
= PROBE HEAT Switches
ON – power is supplied to heat related system.
OFF – power off.
ANTI-ICE & RAIN
737 Sec. 6.3 Page 21
Flight Manual Continental Rev. 11/15/02 #41
BCD Probe Heat Panel
< Probe Heat Lights
Illuminated (amber) – related probe not heated.
= PROBE HEAT Switches
ON – power is supplied to heat related system.
OFF – power off.
ANTI-ICE & RAIN
Sec. 6.3 Page 22 737
Rev. 11/15/02 #41 Continental Flight Manual
INTENTIONALLY LEFT BLANK
ANTI-ICE & RAIN
737 Sec. 6.3 Page 23
Flight Manual Continental Rev. 11/15/02 #41
CONTROLS AND INDICATORS
WINDSHIELD / FOOT AIR CONTROLS
< WINDSHIELD AIR Controls
PULL – Supplies conditioned air to No. 1 windows for defogging.
= FOOT AIR Controls
PULL – Supplies conditioned air to pilots’ leg positions.
ANTI-ICE & RAIN
Sec. 6.3 Page 24 737
Rev. 11/15/02 #41 Continental Flight Manual
INTENTIONALLY LEFT BLANK
ANTI-ICE & RAIN
737 Sec. 6.3 LEP-1
Flight Manual Continental Rev. 11/15/02 #41
LIST OF EFFECTIVE PAGES
PAGE DATE PAGE DATE PAGE DATE
* Asterisk indicates page(s) revised or added by the current revision.
* TOC-1 11/15/02
* TOC-2 11/15/02
* 1 11/15/02
* 2 11/15/02
* 3 11/15/02
* 4 11/15/02
* 5 11/15/02
* 6 11/15/02
* 7 11/15/02
* 8 11/15/02
* 9 11/15/02
* 10 11/15/02
* 11 11/15/02
* 12 11/15/02
* 13 11/15/02
* 14 11/15/02
* 15 11/15/02
* 16 11/15/02
* 17 11/15/02
* 18 11/15/02
* 19 11/15/02
* 20 11/15/02
* 21 11/15/02
* 22 11/15/02
* 23 11/15/02
* 24 11/15/02
* LEP-1 11/15/02
* LEP-2 11/15/02
AUTO FLIGHT
737 Sec. 6.4 TOC-1
Flight Manual Continental Rev. 11/15/02 #41
AUTO FLIGHT
TABLE OF CONTENTS
AUTOMATIC FLIGHT SYSTEM DESCRIPTION ....................................1
General...............................................................................................1
Autopilot Flight Director System (AFDS) ...........................................1
MCP Mode Selector Switches ...........................................................1
Autopilot Engagement Criteria...........................................................2
Autopilot Disengagement...................................................................2
AFS Failures.......................................................................................3
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